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Vortex shedding from a circular cylinder near a moving ground

机译:涡流从移动地面附近的圆柱体上脱落

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摘要

The flow and force characteristics have been experimentally investigated of a circular cylinder with an aspect ratio of 8.33, with and without end-plates, placed near and parallel to a moving ground, on which substantially no boundary layer developed to interfere with the cylinder. Mean drag and lift measurements, surface oil flow visualization, and particle image velocimetry (PIV) measurements were carried out at two upper-subcritical Reynolds numbers of 0.4 and 1.0×105 (based on the cylinder diameter d) to investigate the mechanisms of the ground effect, i.e., the effect of the gap-to-diameter ratio h/d, where h is the gap between the cylinder and the ground. For the cylinder with end-plates, on which the oil flow patterns were observed to be essentially two-dimensional, the drag rapidly decreased as h/d of less than 0.35, unlike that usually observed near a fixed ground. This critical drag behavior was found to be directly related to a global change in the near wake structure of the cylinder; as h/d 0f less than 0.35, unlike that usually observed near a fixed ground. This critical drag behavior was found to be directly related to a global change in the near wake structure of the cylinder; as h/d decreased the Kármán-type vortex shedding became intermittent at h/d=0.4, and then totally ceased and instead two nearly parallel shear layers were formed behind the cylinder at h/d=0.3 and below. For the cylinder without end-plates, however, no such critical change in drag was observed as the Kármán-type vortices were not generated in the near wake region at all h/d investigated. Based on the experimental results obtained, further discussions are also given to the essential cause of the cessation of the Kármán vortex shedding in the ground effect. © 2007 American Institute of Physics.
机译:已经通过实验研究了长宽比为8.33的圆柱体(带有和不带有端板)的圆柱体,该圆柱体放置在靠近并平行于移动地面的位置,在该地面上基本上没有边界层会干扰圆柱体。在两个上亚临界雷诺数分别为0.4和1.0×105(基于圆柱直径d)下进行了平均阻力和升程测量,表面油流可视化以及粒子图像测速(PIV)测量,以研究地面的机理效应,即间隙直径比h / d的效应,其中h是圆柱体与地面之间的间隙。对于带有端板的气缸,其油流模式基本上是二维的,阻力通常以h / d小于0.35的速度迅速减小,这与通常在固定地面附近观察到的阻力不同。发现该临界阻力行为直接与气缸近尾流结构的整体变化有关。 h / d 0f小于0.35,这与通常在固定地面附近观察到的情况不同。发现该临界阻力行为直接与气缸近尾流结构的整体变化有关。当h / d减小时,在h / d = 0.4时,Kármán型涡旋脱落变得断断续续,然后完全停止,取而代之的是在h / d = 0.3及以下时在圆柱体后部形成了两个几乎平行的剪切层。然而,对于没有端板的气缸,没有观察到这种阻力的关键变化,因为在所研究的所有h / d都未在近尾流区域产生Kármán型涡旋。根据获得的实验结果,还进一步讨论了地面效应中停止Kármán涡流脱落的根本原因。 ©2007美国物理研究所。

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